(a)
Remove and discard the lockwire from the knurled sleeve nut (2).
(b)
Carefully loosen the knurled sleeve nut (2) and remove the collets from the cable joint.
(c)
Disconnect the flexible control assembly (1) from the release cable assembly (21).
(2)
In the passenger compartment:
(a)
Remove and discard the cotter pin (3).
(b)
Remove the pin (4) and the washers (5) and disconnect the flexible control assembly (1) from the bellcrank (6).
(c)
Remove and discard the lockwire and loosen the conduit adjust nuts (7) and (8).
(d)
Remove the bolt (9), the washer (10) and the nut (11).
(e)
Remove the bolt (12) and the nut (13) and the flange (14).
(f)
Remove the old sealant from the flange (14), the bolts (9) and
(12) and the nuts (11) and (13).
(g)
Remove and discard the lockwire and loosen the bracket attach nuts (15) and (16).
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CES
Flexible Control Assembly Figure 401/TASK 25-62-43-991-001-A12 (SHEET 1)
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CES
Flexible Control Assembly Figure 401/TASK 25-62-43-991-001-A22 (SHEET 2)
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CES
(h) Remove the screws (17), the washers (18), the nuts (19) and the clamps (20).
(3) Remove the flexible control assembly (1) from the aircraft structure.
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CES TASK 25-62-43-400-001 Installation of the Flexible Control Assembly
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
TLW101 1 TEST TOOL - RELEASE CABLE , ESCAPE SLIDE
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-018 USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
3 cotter pin 25-62-04 10 -070A 3 cotter pin 25-62-04 10A-070
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CES D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
21-20-00-410-001
25-21-41-400-001 25-23-43-400-001 25-23-44-400-001
25-23-47-400-002
25-23-48-400-001 25-62-00-081-001
25-62-00-481-001
52-21-11-000-001 52-21-11-400-001 52-30-00-860-002
25-62-43-991-001-A FOR FIN 5001WM 21-20-00-010-001 25-21-41-000-001 25-23-43-000-001 25-23-44-000-001 25-23-47-000-002
25-23-48-000-001 52-21-11-000-001
3. Job Set-up
__________
Subtask 25-62-43-860-051
Installation of the Air-Conditioning Distribution
Ducts
Installation of the Passenger Seats
Installation of the Upper Sidewall Panel(s)
Installation of the Lower Sidewall-Panels (Dado
Panels)
Installation of the Upper Sidewall Panel Assy 241LW,
(242LW), 241CW, (242CW) and 241FW, (242FW)
Installation of the Cove Light Panels
Special Precautions after Work on the Offwing
Escape-Slide Systems
Special Precautions before Work on the Offwing
Escape-Slide Systems
Removal of the Emergency Exit Hatch
Installation of the Emergency Exit Hatch
Close the FWD or AFT Cargo-Compartment Door with the
Yellow Electric Pump
Fig. 401
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